Investigation of Load and Pressure Distribution onWing with Wake Rollup for Low Speed Aircraft
The presented work shows a preliminary analytic method for estimation of load and pressure distributions on low speed wings with flow separation and wake rollup phenomenas. A higher order vortex panel method is coupled with the numerical lifting line theory by means of iterative procedure including...
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| Formato: | article |
| Lenguaje: | EN |
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Al-Khwarizmi College of Engineering – University of Baghdad
2008
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| Acceso en línea: | https://doaj.org/article/8a28d42d8cdf4b1fbf58ef69310899d3 |
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